Guizhou Soar Dragon. Specifications. A photo.
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Guizhou Soar Dragon. Specifications. A photo.

Guizhou Soar Dragon. Specifications. A photo.

 

Guizhou Soar Dragon - Chinese multifunctional military unmanned aerial vehicle developed by the corporation «Guizhou Aircraft Industry Corporation».

Unmanned aerial vehicle model Guizhou Soar Dragon was designed by experts from the corporation «Guizhou Aircraft Industry Corporation» in 2006 year, the new aircraft is intended for use only in the military sphere, and according to preliminary data, the first of its flight tests were to take place in 2014 year, however, most likely due to the secrecy of the project, the official publicity of these events are not received.

Chinese unmanned aerial vehicle Guizhou Soar Dragon is designed for reconnaissance, patrol and observation flights, carry out special missions and operations associated with monitoring and controlling the area of ​​a potential enemy movements.

Initially it was assumed that the air means Guizhou Soar Dragon will be equipped with their own weapons systems, however, in the final version the developers abandoned the idea.

This unmanned aerial vehicle has a relatively large dimensions, in particular in its length 14 33 centimeters meters, the device has a wingspan integral meter 24 86 centimeters, which in turn requires a specially prepared runway for takeoff and landing.

Power section UAV Guizhou Soar Dragon represented by one turbojet Guizhou WP-13, which is capable of generating thrust in 43,1 kN, which in turn, provides a means of air movement at the maximum speed 870 km \ h., And filter the effective range is 7000 kilometers.

 

Specifications Guizhou Soar Dragon.

 

  • Length: 14,33 m .;
  • Wingspan: 24,86 m .;
  • Height: 5,41 m .;
  • Maximum takeoff weight: unknown;
  • Cruising flight speed: 750 km \ h .;
  • Maximum flight speed: 870 km \ h .;
  • Maximum flight distance: 7000 km .;
  • Maximum flight height: 18000 m .;
  • aircraft engine type: turbojet;
  • Powerplant: Guizhou WP-13;
  • Power: 43.1 kN. 

 

 

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